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AISI 202 Stainless Steel vs. 6151 Aluminum

AISI 202 stainless steel belongs to the iron alloys classification, while 6151 aluminum belongs to the aluminum alloys. There are 30 material properties with values for both materials. Properties with values for just one material (3, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is AISI 202 stainless steel and the bottom bar is 6151 aluminum.

Metric UnitsUS Customary Units

Mechanical Properties

Elastic (Young's, Tensile) Modulus, GPa 200
69
Elongation at Break, % 14 to 45
1.1 to 5.7
Fatigue Strength, MPa 290 to 330
80 to 100
Poisson's Ratio 0.28
0.33
Shear Modulus, GPa 77
26
Shear Strength, MPa 490 to 590
190 to 200
Tensile Strength: Ultimate (UTS), MPa 700 to 980
330 to 340
Tensile Strength: Yield (Proof), MPa 310 to 580
270 to 280

Thermal Properties

Latent Heat of Fusion, J/g 290
410
Maximum Temperature: Mechanical, °C 910
170
Melting Completion (Liquidus), °C 1400
650
Melting Onset (Solidus), °C 1360
590
Specific Heat Capacity, J/kg-K 480
900
Thermal Conductivity, W/m-K 15
170
Thermal Expansion, µm/m-K 17
23

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 2.4
45
Electrical Conductivity: Equal Weight (Specific), % IACS 2.9
150

Otherwise Unclassified Properties

Base Metal Price, % relative 13
9.5
Density, g/cm3 7.7
2.7
Embodied Carbon, kg CO2/kg material 2.8
8.2
Embodied Energy, MJ/kg 40
150
Embodied Water, L/kg 150
1180

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 120 to 260
3.5 to 18
Resilience: Unit (Modulus of Resilience), kJ/m3 250 to 840
520 to 580
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 25
50
Strength to Weight: Axial, points 25 to 35
34
Strength to Weight: Bending, points 23 to 29
39
Thermal Diffusivity, mm2/s 4.0
70
Thermal Shock Resistance, points 15 to 21
15

Alloy Composition

Aluminum (Al), % 0
95.6 to 98.8
Carbon (C), % 0 to 0.15
0
Chromium (Cr), % 17 to 19
0.15 to 0.35
Copper (Cu), % 0
0 to 0.35
Iron (Fe), % 63.5 to 71.5
0 to 1.0
Magnesium (Mg), % 0
0.45 to 0.8
Manganese (Mn), % 7.5 to 10
0 to 0.2
Nickel (Ni), % 4.0 to 6.0
0
Nitrogen (N), % 0 to 0.25
0
Phosphorus (P), % 0 to 0.060
0
Silicon (Si), % 0 to 1.0
0.6 to 1.2
Sulfur (S), % 0 to 0.030
0
Titanium (Ti), % 0
0 to 0.15
Zinc (Zn), % 0
0 to 0.25
Residuals, % 0
0 to 0.15